479.575 PEOPLE
People | Locations | Statistics |
---|---|---|
Ziakopoulos, Apostolos | Athens |
|
Vigliani, Alessandro | Turin |
|
Catani, Jacopo | Rome |
|
Statheros, Thomas | Stevenage |
|
Utriainen, Roni | Tampere |
|
Guglieri, Giorgio | Turin |
|
Martínez Sánchez, Joaquín |
| |
Tobolar, Jakub |
| |
Volodarets, M. |
| |
Piwowar, Piotr |
| |
Tennoy, Aud | Oslo |
|
Matos, Ana Rita |
| |
Cicevic, Svetlana |
| |
Sommer, Carsten | Kassel |
|
Liu, Meiqi |
| |
Pirdavani, Ali | Hasselt |
|
Niklaß, Malte |
| |
Lima, Pedro | Braga |
|
Turunen, Anu W. |
| |
Antunes, Carlos Henggeler |
| |
Krasnov, Oleg A. |
| |
Lopes, Joao P. |
| |
Turan, Osman |
| |
Lučanin, Vojkan | Belgrade |
|
Tanaskovic, Jovan |
|
Kozakiewicz, Adam
in Cooperation with on an Cooperation-Score of 37%
Topics
- aircraft
- turbine
- compressor
- air intake
- turbine engine
- assessment
- modeling
- simulation
- airport
- duct
- pressure
- propeller blade
- airplane
- stator
- jet propelled aircraft
- engine operation
- numerical analysis
- vortex
- jet engine
- surging
- stall
- pressure field
- propulsion
- weapon
- optimisation
- airfoil
- drone
- vibration
- aerodynamic
- examination
- fuselage
- gust
- engineering
- engine
- show 4 more
Publications (13/13 displayed)
- 2022Areas of Investigation into Air Intake Systems for the Impact on Compressor Performance Stability in Aircraft Turbine Enginescitations
- 2022Determination of Ranges of Unstable Operation of Axial Compressor for Aircraft Turbine Engines
- 2022Intake System Performance Stability as a Function of Flow Throttling
- 2021ELECTRIC AIRCRAFT PROPULSION
- 2018Main problems of the evaluation and selection of advanced weapon systems exemplified by a multi-role combat aircraftcitations
- 2016A unified method of identification and optimization of airfoils for aircrafts, turbine and compressor blades
- 2015Modeling of an Unmanned Aerial Vehicle (UAV) Body for the Needs of Numerical Aerodynamic Investigations, Strength Analysis and Examinations of Free Vibrationscitations
- 2015Modeling of an Unmanned Aerial Vehicle (UAV) Body for the Needs of Numerical Aerodynamic Investigations, Strenght Analysis and Examinations of Free Vibrationscitations
- 2013Analysis Of The Gust Impact On Inlet Vortex Formation Of The Fuselage-Shielded Inlet Of An Jet Engine Powered Aircraft
- 2013Application of CAD/CAM/CAE Systems to the Process of Aircraft Structures Analysis by Means of Reverse Engineering Methods
- 2013Unified Method of Identification and Optimization of Airfoils for Aircrafts, Turbine and Compressor Blades
- 2013Unstable operation of the turbine aircraft engine
- 2011Construction of an air intake system model for F-100-PW-229 engine in F-16 aircraft for intake vortex development analysis
Places of action
article
Analysis Of The Gust Impact On Inlet Vortex Formation Of The Fuselage-Shielded Inlet Of An Jet Engine Powered Aircraft
Topics
Search in FID move catalog